[IGSREPORT-28785] Wk 2216 IGS Final Orbits
acc
acc at igs.org
Fri Jul 15 11:07:55 UTC 2022
Author: AC Coordinator / GA MIT
sum-file Version 2.0
Final IGS Orbit Combination - Week 2216 (Jun 26, 2022 - Jul 02, 2022)
Contacts: acc at igs.org
COMBINATION STRATEGY:
---------------------
Starting with GPS week 860, the IGS Final orbit combination is done directly
in the ITRF without any alignment to the Bulletin B EOP series.
Each centre satellite clock corrections are first transformed to a common
reference. One of the following two methods can be used (the REMARKS section of
this report gives which method is used):
[1] For each centre, a clock offset and a drift are estimated with respect to
the broadcast clock corrections using only non-SA satellites;
[2] A chosen reference centre is aligned to the broadcast clock corrections
using all satellites. All other centres are then aligned to that reference
centre.
The offsets and drifts are used to align each centre satellite clock
corrections to GPS time. Ephemerides and clock corrections are then combined
as weighted averages computed over all centres. Each centre is given a
position weight and a clock weight. The position weights are computed from
each centre's absolute deviation to the unweighted average orbit after the
estimation of a 7-parameter Helmert transformation. The clock weights are
either computed from [1] the absolute deviation of the initial alignment to
broadcast clock for the non-SA satellites, or [2] from the absolute deviation
of centre's aligned clock corrections with respect to the unweighted mean.
Finally, a 7-parameter Helmert transformation and clock offset and drift are
estimated for each centre with respect to the combined solutions and parameters
and RMS of fit reported. All the above estimations are performed using the
L1-norm robust scheme.
Each centre ephemerides are also evaluated individually and independently from
the orbit combination by using week long arcs. The Earth Orientation Parameters
(EOP) used in this evaluation are those submitted by the respective centres.
The IGS combined orbits/clocks and all centres providing both orbit and clock
solutions are further evaluated by an independent point positioning (navigation)
program that uses both phase and pseudorange data at each SP3 epoch. This is
primarily intended for testing clock solution precision as well as the
orbit/clock consistency.
Like the clock solutions broadcast in the navigation message, the combined
satellite clocks are corrected for the periodical relativistic correction (see
e.g. GPS interface Control document ICD-GPS-200, p.73):
-2*(X.V)/c [distance unit],
where X and V are the inertial sv state and velocity vectors and c is the speed
of light. Also for compatibility with broadcast GPS time, the IGS clocks use
the linear combination of phase-smoothed P1 and P2 pseudorange data to remove
the 1st order ionospheric delay, with no other delay calibrations applied.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
PRODUCTS GENERATED:
-------------------
The resulting average ephemeris and clocks are output to daily files in SP3
format. The satellite accuracy codes displayed in the header are based on the
weighted RMS for each satellite over each daily arc. Note that each file
contains all the satellites that appear in any of the centre ephemeris files.
If a satellite or centre was excluded from combination, a note in the REMARKS
section of this report will identify the exclusion and the reason.
The resulting x and y earth rotation parameters (ERP) associated with the IGS
ephemeris files and their rates (xrt, yrt) are computed using a weighted average
of all available centres (as part of the separate SINEX combination since GPS
week 1051; weighted according to the orbit combination before that time).
Starting with GPS wk 0894, IGS LOD combinations were implemented in the
Final IGS solutions. AC LOD biases with respect to Bulletin A are estimated
using Bulletin A most recent 10 days, i.e. up to 5 days prior to the last
non-predicted day of Bulletin A. AC LOD biases are removed and the new AC
bias-free LODs are used to compute a weighted IGS LOD which in turn is
integrated into IGS UT1-UTC. The starting UT1-UTC value is chosen as Bulletin
A fifth day prior to its last non-predicted day. Both IGS LOD and UT1-UTC
values are printed in the IGS Final erp file.
The Final Orbit files generated and uploaded into CDDIS @ NASA/GSFC are:
igs2216[0-6].sp3 IGS GPS ephemeris files in SP3 format.
igs2216[0-6].clk IGS GPS satellite and station clocks in clock RINEX format.
igs2216[0-6].cls IGS GPS clock combination summary report.
igs22167.erp Earth Rotation Parameters (ERP) and their rates as well as
Universal Time (UT1-UTC) and Length Of Day (LOD) associated
with IGS ephemerides.
igs22167.sum Complete report.
REMARKS concerning the IGS Orbit Combination:
---------------------------------------------
1. The centres used in the clock combination are COD, EMR, ESA, GFZ, GRG, MIT, and
JPL. The other centres are excluded because of poorer consistency, they provide
broadcast clocks, or clock corrections are not provided (SIO). The clock
information not used is still compared to the combination for completeness. The
value of 999999.999999 microseconds, according to the SP3 format convention,
signifies that no clock solution is available and therefore must not be used.
In general, if an AC does not contribute to the terrestrial reference frame
(i.e. the SINEX combination), then any corresponding orbits & clocks
contributed from that AC should not be included with weight in this
combination. This is done to ensure a high level of consistency between the TRF
and the orbital frame. However, there is an exception for the clocks if the AC
is the reference center. In that case, only the clocks from that AC are
included with weight.
Starting week 1707:
cod = cof${wwww}[0-6].[clk,snx,sp3] & cod = cof${wwww}7.[erp,sum]
2. Rapid (IGR) orbits/clocks are included in the combination for statistics only.
Starting week 1582, a new orbit solution from CNES/GRGS (GRG) is included with
weight. GRG clocks are included with weight starting 12-Aug-2012 (GPS Week
1701, day 0, MJD 56151), after a procedural change to generate estimates in
the center-of-figure frame instead of the center-of-mass frame. GRG LOD
estimates are included for comparison only.
3. The following centre clock solutions, which provide broadcast clock
corrections, were excluded from the combination but kept in the combination
statistics:
-> Centre: NGS
4. The following clock solutions were excluded from the combination because they
were biasing the combined clock solutions (clock shifts/outliers) but were
kept for the RMS computation. Duplicate entries can arise due to separate
combination runs for the 30-s clocks ACs (listed first) and the 5-min clock
ACs (listed second).
Day | Centre | PRN/STA list
----+--------+---------------
0 | EMR | CHUR FAIR
0 | ESA | YEL2 CZTG GAMB YEL2
0 | GFZ | HERS POHN HERS POHN
0 | GRG | NNOR SGOC SVTL LHAZ NNOR SGOC SVTL
0 | JPL | ASCG BJFS BRFT CHTI CPVG CZTG GAMB HYDE KERG KZN2
0 | JPL | LHAZ MCIL PARC RIOP SSIA STK2 SYOG TRO1 ZECK HYDE
0 | JPL | KZN2 SYOG ZECK
1 | EMR | CHUR CHUR TSKB
1 | ESA | DAV1 SYOG YEL2 DAV1 SYOG YEL2
1 | GFZ | 17 17 DAV1 HERS POHN DAV1 HERS POHN
1 | GRG | 17 17 HYDE SVTL GAMB HYDE SVTL
1 | JPL | 20 POHN SYOG FLIN SYOG
2 | ESA | PTBB CZTG PTBB
2 | GFZ | 28 28 HERS POHN HERS POHN
2 | GRG | 17 IRKJ IRKJ
2 | JPL | ASCG BJFS CHUR CPVG CUSV CZTG FALK LHAZ LMMF MCIL
2 | JPL | NICO POHN RIOP STK2 XMIS
3 | GFZ | SAVO SAVO
3 | GRG | 28 28 SVTL SVTL WIND
3 | JPL | ASCG BRFT CHTI CHUR CNMR CPVG CZTG GAMB HNLC HOFN
3 | JPL | KERG MCIL NYA1 OHI3 RIOP STK2 THTI UFPR CHUR CZTG
3 | MIT | 28
4 | COD | ABMF ABMF
4 | EMR | TSKB
4 | ESA | 28 28 NYA1 NYA1
4 | GFZ | 28 28 TRO1 TRO1
4 | GRG | SVTL SVTL TRO1
4 | JPL | ASCG BADG BJFS CKIS CPVG CUSV CZTG DJIG FALK GAMB
4 | JPL | LHAZ MBAR MCIL MQZG NYA1 OHI3 POLV RIOP SAMO SAVO
4 | JPL | THTI XMIS BADG GAMB
5 | COD | AREQ AREQ
5 | EMR | USUD
5 | ESA | DAV1 GAMB DAV1 GAMB
5 | GFZ | AREQ DAV1 SYOG USUD AREQ DAV1 SYOG
5 | GRG | GLSV WIND GLSV WIND
5 | JPL | BADG BADG CZTG NICO
6 | COD | DAV1 DAV1
6 | EMR | FAIR WHIT
6 | ESA | FLIN QAQ1 FLIN QAQ1
6 | GFZ | 28 28 DAV1 DAV1
6 | GRG | SGOC SGOC
6 | JPL | ASCG CHTI GAMB KERG MCIL QAQ1 SAVO STK2 SYOG FAIR
5. New clock offsets and drifts were estimated for centres showing reference
clock resets. Note that only the largest clock offset and drift are output
to the summary file. However, the clock combination and the listed RMS
include all the clock segments. In summary, the following clock
shifts/resets were noticed and accounted for:
Day | Centre | Time | Jump
----+--------+--------+-------------
1 | JPL | ~22:15 | ~ -0.19 ns
5 | JPL | ~23:10 | ~ 0.19 ns
6. Starting on 22-Oct-2000 (GPS Week 1085-0; MJD=51839) all IGS clock products
are based on the new clock combination scheme which uses the clock RINEX
files as input if available, otherwise SP3 clocks are used. The AC clocks are
corrected for the radial offsets of their satellite orbits compared to the
combination.
7. The following table lists all maneuvered satellites for this week. The
solutions from COD and ESA, which modeled the maneuver, are used that day for
combination, if available. An associated accuracy code of 0 (unknown) is given
if only one AC is left (no redundancy). For the long arc evaluation the arc is
split into two parts at the given maneuver epoch.
PRN | Date | Ref. NANU
----+------------+----------
G08 | 2022_06_30 | 2022032
8. Velocity changes were estimated to alleviate the effects of modeling problems,
experienced by all centres,in the Long Arc (LA) process.
Velocity changes per day and affected satellites:
Day | 0 | 1 | 2 | 3 | 4 | 5 | 6 |
--------+----+----+----+----+----+----+----+
PRN G08 | 4 | 4 | 4 | 4 | 4 | | |
PRN G32 | | | | | 4 | 4 | 4 |
9. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) all IGS products, including the IGS combined
orbits, are based on the IGS realization of the ITRF2005 reference frame
(IGS05). For more information see IGSMAIL #5447. The IGS05 frame is also the
basis for the homogeneously reprocessed IGS products from GPS Weeks 730 to 1459
(1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) all IGS products, are
based on the IGS realization of the ITRF2008 reference frame (IGS08). For more
information see IGSMAIL #6354.
Starting 07-Oct-2012 (GPS Week 1709, day 0, MJD 56207) all IGS products, are
based on the updated IGS08 frame (IGb08). For more information see IGSMAIL
#6663.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) all IGS products,
are based on the IGS realization of the ITRF2014 reference frame (IGS14).
For more information see IGSMAIL #7399.
Starting 17-May-2020 (GPS Week 2106, day 0, MJD 58986) all IGS products,
are based on the updated reference frame (IGb14).
For more information see IGSMAIL #7921.
10. Small rotations were applied to all the AC orbit and ERP values in order to
align them to the current IGS reference frame. These RX, RY and RZ rotations
were estimated in the IGS SINEX combination process, performed by the IGS
Reference Frame Coordinator at the Institut Geographique National (IGN).
Starting on 19-Aug-2012 (GPS Week 1702; MJD=56158), ACs began contributing
products based on 1d SINEX integrations. As a result, the SINEX combinations
are now done daily instead of weekly, and the associated daily rotations are
applied here to the orbits and ERPs. The estimated 7 transformations, from
which only the 3 rotations are applied to the orbit and ERP values, are:
| | DX DY DZ RX RY RZ SCL
Centre | Day | [mm] [mm] [mm] [uas] [uas] [uas] [ppb]
-------+-----+---------------------------------------------------
COD | 0 | .2 -.0 .5 2 -1 2 -.25
EMR | 0 | -2.0 -.1 1.9 -33 -19 -11 .04
ESA | 0 | -1.4 -1.6 -.4 -24 12 28 -.37
GFZ | 0 | .1 -.3 .9 2 5 4 -.32
GRG | 0 | -.9 -1.9 -21.7 -17 6 -34 .25
JPL | 0 | -.7 -6.7 .9 -4 14 -13 .15
MIT | 0 | -6.3 -.6 -10.0 -2 20 -26 .13
NGS | 0 | -.5 -5.9 1.5 -38 19 3 -.11
SIO | 0 | -4.2 -.9 -8.9 -49 113 -60 .05
COD | 1 | .1 .0 .3 1 0 -2 -.19
EMR | 1 | -1.5 -5.7 -10.5 -29 -21 4 .14
ESA | 1 | -1.2 -1.2 -.9 -17 0 41 -.30
GFZ | 1 | .4 -.4 .3 1 -9 3 -.22
GRG | 1 | 3.6 -3.5 -23.1 -5 -3 -10 .09
JPL | 1 | 4.2 -3.6 -9.5 -2 -1 9 -.23
MIT | 1 | -3.8 2.6 -12.6 -13 5 4 .12
NGS | 1 | 2.5 -2.6 -7.5 -25 -13 31 -.08
SIO | 1 | -4.7 1.6 -12.2 -30 146 -34 -.06
COD | 2 | .2 .0 .4 1 -1 -2 -.25
EMR | 2 | -2.9 1.4 -4.0 -11 -20 -2 .08
ESA | 2 | -1.9 -1.7 -.8 -19 15 52 -.25
GFZ | 2 | .1 -.4 .4 -1 -14 12 -.16
GRG | 2 | 2.1 -1.2 -14.4 -12 -10 -27 .08
JPL | 2 | 2.8 -1.3 -5.1 0 6 -9 -.06
MIT | 2 | -.6 2.9 -11.1 1 -3 3 .03
NGS | 2 | -3.1 -2.9 1.3 -3 9 13 -.16
SIO | 2 | -2.5 3.5 -10.6 -14 105 35 -.16
COD | 3 | .1 -.1 .3 0 -2 5 -.24
EMR | 3 | 4.9 1.7 -1.7 -34 -7 25 -.01
ESA | 3 | -2.0 -1.8 -1.6 -22 7 62 -.43
GFZ | 3 | .5 -.4 .5 6 -11 7 -.45
GRG | 3 | 2.9 2.3 -19.9 -9 -18 -32 -.08
JPL | 3 | 2.0 -4.5 -5.1 6 7 -15 -.17
MIT | 3 | -1.2 1.8 -13.4 -17 -5 -3 -.13
NGS | 3 | -2.1 1.8 -11.0 3 -26 -2 -.28
SIO | 3 | -3.4 4.2 -11.0 -3 136 44 -.13
COD | 4 | .2 .1 .3 -1 -1 2 -.32
EMR | 4 | -4.7 -2.7 -8.7 -25 -13 1 .27
ESA | 4 | -1.6 -2.5 -1.5 -12 21 46 -.38
GFZ | 4 | .1 -.3 .3 14 -2 17 -.26
GRG | 4 | .4 .4 -21.5 -9 -7 -11 .21
JPL | 4 | -.7 -2.4 .8 -3 4 11 .01
MIT | 4 | -5.3 2.5 -15.9 -20 3 5 .14
NGS | 4 | -1.0 -5.7 -11.8 -8 -1 19 -.13
SIO | 4 | -6.4 1.5 -13.8 -22 161 14 -.01
COD | 5 | .1 -.1 .3 1 -6 5 -.22
EMR | 5 | -1.2 -4.7 -3.2 -19 -15 2 .20
ESA | 5 | -1.5 -2.2 -.7 -28 -6 51 -.33
GFZ | 5 | .5 -.9 .3 -3 -17 20 -.32
GRG | 5 | 2.4 -1.9 -17.4 -7 -1 -8 .10
JPL | 5 | 2.8 -7.5 -2.6 0 0 0 -.12
MIT | 5 | -.5 1.7 -13.0 -18 6 -12 .07
NGS | 5 | 1.4 -7.4 -.3 -13 9 30 -.08
SIO | 5 | -4.4 2.2 -7.3 -5 84 47 .08
COD | 6 | .2 .4 .5 6 -1 1 -.21
EMR | 6 | -4.0 -3.4 -6.1 -32 -37 26 .12
ESA | 6 | -1.3 -2.0 -.6 -22 -7 60 -.25
GFZ | 6 | .0 -.8 .0 -9 -21 27 -.20
GRG | 6 | .9 -1.3 -13.2 -8 -16 -3 .27
JPL | 6 | 5.1 -4.1 -4.2 -12 -13 12 .23
MIT | 6 | -1.3 3.5 -14.5 -30 -2 2 .20
NGS | 6 | 8.2 .6 -3.2 -16 -17 16 -.04
SIO | 6 | -1.6 4.4 -9.5 9 100 80 -.02
11. As inidicated in the previous remarks, the IGS final orbits are aligned to the
IGS reference frame by pre-aligning each AC orbit with the 3 corresponding
SINEX rotations. This approach began 27-Feb-2000 (GPS Week 1051-0; MJD 51601).
Starting sometime prior to 19-Aug-2012 (GPS Week 1702; MJD=56158), the orbit
combination procedures used an incorrect sign convention to apply the SINEX
RX and RY values to the AC orbits.
Also starting 27-Feb-2000 (GPS Week 1051-0; MJD 51601), the AC orbits were
pre-aligned using rotations derived from differences between AC and IGS
combined x and y polar motion. These ERP rotations were intended to
approximate day-to-day variations of the AC orbital frames when only weekly
averaged AC TRF rotations were available (For more details, see IGSMAIL
#2750). With the change to daily SINEX integrations starting 19-Aug-2012, the
ERP rotations are no longer needed/applied.
12. Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011 (GPS
Week 1631, day 6, MJD 55667) the absolute antenna model is introduced (IGSMAIL
#5438). The antenna phase center offsets and phase center variations are given
in the file:
https://files.igs.org/pub/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
https://files.igs.org/pub/station/general/igs08.atx
The JPL solution did not use IGS08/igs08.atx until GPS Week 1649, which caused
their RMS clock residuals to be higher during that period than for the other
centres; from GPS Week 1632 through 1648 the JPL solution is excluded from the
weekly SINEX combination.
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
https://files.igs.org/pub/station/general/igs14.atx
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Most combination statistics are with respect to the combined orbits and
consist of seven parts. The first, Table 1, summarizes all statistics for
the week. It contains means and standard deviations over the week of
satellite ephemeris and clock correction transformation parameters for
each centre (Table 1.2216.a). It also displays the computed satellite
position sigmas for the combined orbits (Table 1.2216.b).
The second part, Table 2, contains the complete ephemeris and clock
correction transformation parameters (includes both the apriori and a
posteriori values) for each centre and each day (Tables 2.2216.[0-6]).
The third part, Table 3, contains two types of daily RMS for each satellite
and centre, along with the computed satellite position sigmas for the
combined orbits (Tables 3.2216.[0-6]). The first type of satellite RMS is
based on orbit combination and the second RMS type is a result of the 7-day
arc evaluation of each centre ephemerides. The fourth part, Table 4, is a
weekly summary of the daily precise navigation summaries for centres
providing both orbit and clock solutions. It contains weekly station RMS
w.r.t. the initial coordinates for the Latitude, Longitude and Height
components for up to three IGS stations (Table 4.1307). The fifth part,
Table 5, is similar to Table 4 and contains daily precise navigation
statistics (Tables 5.2216.0-6). The sixth part, Table 6, is a weekly
summary of daily ERP combination statistics. The seventh part, Table 7,
contains the daily ERP statistics. But this is not the IGS official ERP
combination products (which come from the accompanying SINEX combination)
but provided to check combination consistency, etc.
In Tables 1-3, the most important statistic which is meaningful for intra
centre/satellite analysis is labeled WRMS. It is a weighted RMS where
normalized weights are based on accuracy codes given in the SP3 files, and
should not be affected by downweighted/problem satellites when acknowledged
by individual centres in their SP3 file.
Table 1: Week 2216 summary. (Jun 26, 2022 - Jul 02, 2022)
Table 1.2216.a GPS week: 2216 MJD: 59756.000-59762.000
Mean and standard deviations of transformation parameters to the
combined IGS orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 669| 0 0 0 18 -20 16 -.01 7 7 | -812 287 7 87
| 0 0 1 10 10 12 .01 | 199 211
emr 80| -3 1 2 25 -3 0 .01 13 13 | 202257 -721 17 118
| 0 2 1 13 16 13 .02 | 2257 619
esa 150| 0 0 1 -8 -3 2 -.04 8 8 | -1510 735 7 86
| 0 0 1 12 12 10 .01 | 362 445
gfz 238| 0 0 1 6 -26 7 .14 12 12 | 5 145 13 105
| 0 0 2 9 13 15 .04 | 263 345
grg 123| 4 0 -4 0 11 6 -.05 11 10 | -175 136 9 131
| 0 0 3 8 16 13 .03 | 191 236
igr n/a| 0 0 1 10 -17 -5 .01 5 4 | 64547 112466 12 1233
| 0 0 0 6 11 13 .01 | 161092 299060
jpl 80| 0 0 2 -1 -19 -9 .13 9 9 | -1831 -606 8 125
| 0 0 0 10 17 15 .03 | 2067 711
mit 372| 0 0 -1 -17 -3 -13 -.03 7 6 | 63537 112542 29 1738
| 0 0 0 14 14 11 .01 | 161261 298742
ngs 210| 0 0 0 2 13 -5 -.08 9 9 | -268 -102 817 1730
| 0 0 3 8 17 13 .02 | 1611 805
sio 541| 0 0 -1 3 52 9 -.02 9 8 | --- --- --- ---
| 0 0 1 19 38 48 .02 | --- ---
Table 1.2216.b GPS week : 2216 MJD: 59756.000-59762.000
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
1 | 3 3 3 2 3 3 3 |
2 | 3 3 3 3 2 2 3 |
3 | 3 3 3 3 4 4 4 |
4 | 3 3 3 3 3 3 3 |
5 | 3 3 3 4 3 3 4 |
6 | 3 3 3 2 2 2 2 |
7 | 3 2 2 3 2 2 2 |
8 | 3 3 7 4 0 4 3 |
9 | 3 3 3 2 2 3 2 |
10 | 3 3 4 4 4 4 4 |
11 | 4 4 4 4 4 4 4 |
12 | 3 3 3 3 3 3 3 |
13 | 3 3 3 3 3 3 3 |
14 | 5 4 4 4 4 4 4 |
15 | 3 3 3 3 3 3 3 |
16 | 6 5 5 5 4 5 4 |
17 | 3 3 3 3 3 3 3 |
18 | 4 4 4 4 4 4 4 |
19 | 4 4 3 3 3 3 3 |
20 | 4 6 5 4 4 3 3 |
21 | 3 4 3 3 3 3 4 |
22 | 3 3 3 3 3 3 3 |
23 | 6 5 5 5 6 6 8 |
24 | 3 3 3 3 3 3 3 |
25 | 3 3 3 3 3 3 3 |
26 | 4 3 3 3 3 4 4 |
27 | 4 3 3 4 3 4 4 |
28 | 4 4 4 4 5 3 4 |
29 | 3 3 3 3 3 3 3 |
30 | 3 3 3 3 3 3 3 |
31 | 3 3 2 3 2 2 3 |
32 | 3 3 3 3 3 3 3 |
Table 2: Daily transformation of each centre to the combined IGS orbit and
clocks for each day of the week. The transformation displayed is the
result of the combination after the AC orbits were pre-aligned using
the SINEX rotations from above. Prior to Wk 1702, AC ERP rotations
used in the pre-alignment were also displayed.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.2216.0 GPS week: 2216 Day: 0 MJD: 59756.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 663| 0 0 -1 28 -17 34 -.01 8 8 | -794 145 7 86
emr 80| -3 1 4 16 6 9 -.01 14 14 | 205320 -453 17 130
esa 150| 0 0 0 -24 7 5 -.04 8 8 | -1792 1029 7 71
gfz 237| 0 0 2 -3 -31 4 .09 12 12 | 174 113 13 101
grg 125| 3 -1 -6 -15 -2 29 -.07 11 9 | -194 194 9 120
igr n/a| 0 0 0 -1 -17 10 .02 5 5 | 5794 -277 13 126
jpl 80| 0 0 2 10 -21 -19 .14 8 8 | 973 -307 10 127
mit 372| -1 0 0 5 -9 0 -.02 9 8 | 5032 -114 32 1768
ngs 214| 2 0 7 -2 6 -3 -.04 9 9 | -773 81 883 1707
sio 544| 0 0 -4 -10 54 -49 -.00 9 8 | --- --- --- ---
Table 2.2216.1 GPS week: 2216 Day: 1 MJD: 59757.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 669| 0 0 2 5 -24 17 -.01 8 7 | -788 100 6 92
emr 80| -2 -2 1 34 -31 13 -.01 13 13 | 204841 -1802 19 124
esa 150| 0 0 0 6 -18 13 -.02 8 8 | -1576 1043 9 132
gfz 240| 0 0 0 21 -36 33 .14 12 14 | 88 -140 14 108
grg 122| 5 0 -7 0 -6 12 -.03 11 10 | -52 -143 10 140
igr n/a| 0 0 0 11 -36 7 .00 4 4 | 5440 -1311 13 110
jpl 80| 1 -1 1 0 -42 3 .14 10 10 | 505 -1759 9 137
mit 372| 0 0 0 -20 22 -14 -.02 7 7 | 4025 -1093 45 1848
ngs 212| 0 1 0 3 4 9 -.09 9 8 | -910 265 889 1862
sio 550| 0 0 0 -16 95 -61 -.00 8 8 | --- --- --- ---
Table 2.2216.2 GPS week: 2216 Day: 2 MJD: 59758.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 673| 0 -1 0 16 -36 14 -.02 7 7 | -942 604 8 88
emr 80| -4 3 3 29 23 5 .03 14 14 | 202888 -497 17 147
esa 150| 0 0 3 -15 17 13 -.04 9 9 | -1997 1299 7 78
gfz 236| 0 0 5 1 -21 0 .09 12 11 | -507 665 13 106
grg 122| 4 0 -6 4 42 12 -.05 10 9 | -589 500 9 133
igr n/a| 0 0 1 3 0 2 .02 5 5 | 3977 2 14 130
jpl 80| 0 0 1 -10 10 8 .18 9 9 | -1272 -271 8 126
mit 372| 0 0 -2 -4 -14 -23 -.04 7 6 | 2943 240 33 1794
ngs 207| 0 0 0 6 27 -21 -.10 10 9 | -985 556 1090 2086
sio 542| 0 0 -1 -7 -19 10 -.03 9 8 | --- --- --- ---
Table 2.2216.3 GPS week: 2216 Day: 3 MJD: 59759.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 678| 0 0 1 34 -8 12 -.02 7 7 | -897 163 9 87
emr 80| -1 4 5 27 -9 0 .01 13 13 | 202243 -1127 18 122
esa 150| -1 0 0 -8 -4 3 -.04 8 8 | -1647 813 6 66
gfz 241| 0 0 3 -4 -4 7 .13 10 11 | 90 425 12 101
grg 121| 5 -1 -5 -2 15 -2 -.07 12 10 | -83 239 10 136
igr n/a| 0 0 1 14 -6 -10 .02 4 4 | 3812 -774 12 108
jpl 80| 0 0 1 1 -32 -27 .14 8 8 | -1816 -1157 9 120
mit 372| 0 0 -1 -12 3 -6 -.04 7 6 | 2653 -406 20 1579
ngs 212| 0 0 -4 -13 -13 -10 -.07 9 8 | -810 -583 901 1791
sio 550| 0 0 0 0 48 37 -.02 9 8 | --- --- --- ---
Table 2.2216.4 GPS week: 2216 Day: 4 MJD: 59760.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 672| 0 0 1 11 -25 7 -.01 6 6 | -1109 556 7 87
emr 80| -3 1 1 14 -3 0 -.02 13 13 | 200960 -891 18 107
esa 150| 0 0 1 8 -4 -7 -.03 8 8 | -956 -11 7 78
gfz 241| 0 -1 1 15 -16 17 .15 14 13 | 129 74 13 111
grg 125| 4 0 -3 10 10 -3 .01 11 9 | -160 302 9 126
igr n/a| 0 0 1 17 -26 -7 .00 4 4 | 2948 -1008 11 109
jpl 80| 0 0 3 2 -14 3 .12 8 8 | -2970 -776 6 130
mit 372| 0 0 -2 -38 -19 -15 -.03 6 5 | 1773 -874 21 1903
ngs 209| 0 1 0 14 23 0 -.08 10 9 | 3382 -1728 536 1526
sio 548| 0 -1 0 7 85 17 -.01 10 8 | --- --- --- ---
Table 2.2216.5 GPS week: 2216 Day: 5 MJD: 59761.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 665| 0 0 1 22 -22 -2 .00 7 7 | -490 129 7 85
emr 80| -2 1 1 8 -10 3 .04 13 13 | 200036 -406 17 116
esa 150| 0 0 2 -9 -13 2 -.03 8 8 | -1138 427 6 107
gfz 237| 0 0 -1 5 -32 3 .21 13 13 | 251 -371 14 111
grg 125| 5 0 -3 -7 6 -10 -.07 11 10 | -32 -44 9 126
igr n/a| 0 0 0 12 -18 -11 .01 5 4 | 429846 790670 12 7933
jpl 80| 0 0 3 -21 -9 -11 .14 8 8 | -3773 -441 7 126
mit 372| 0 0 -2 -23 3 -32 -.04 8 6 | 429220 790026 25 1868
ngs 208| 0 0 0 5 39 10 -.09 9 8 | -827 283 606 1480
sio 529| -1 0 -3 40 33 49 -.05 10 7 | --- --- --- ---
Table 2.2216.6 GPS week: 2216 Day: 6 MJD: 59762.000
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod 664| 0 0 0 9 -6 28 .01 7 7 | -668 313 7 89
emr 80| -3 0 2 48 0 -29 .01 13 13 | 199515 125 17 82
esa 150| 0 0 2 -15 -8 -13 -.05 9 8 | -1470 548 8 73
gfz 236| 0 1 -1 10 -42 -16 .17 13 12 | -188 254 14 97
grg 125| 4 0 1 7 9 8 -.05 11 10 | -119 -92 10 141
igr n/a| 0 0 1 15 -18 -28 .01 4 4 | 12 -36 12 119
jpl 80| -1 -2 1 3 -25 -27 .07 9 9 | -4469 465 8 115
mit 372| 0 0 -2 -27 -10 -3 -.03 7 6 | -887 19 28 1406
ngs 211| 1 0 -1 1 8 -20 -.09 9 9 | -959 412 815 1661
sio 530| 0 0 0 11 68 64 -.00 11 8 | --- --- --- ---
Table 3: Daily fit for each satellite and each centre resulting from weighted
average combination and from long arc orbit dynamics (7-day). The
first IGS column gives resulting satellite accuracy measures found in
SP3 header. The last IGS column gives the RMS fit of the IGS orbit
when processed through the 7-day arc evaluation.
"E" stands for eclipsing satellites (earth).
"M" stands for eclipsing satellites (moon).
"X" stands for excluded from the statistics but included in IGS orbit.
"T" stands for Total long arc orbit RMS for all satellites.
"NE" stands for long arc orbit RMS for Non-Eclipsing satellites only.
"MEDI" stands for median of the centre's satellite RMS.
"MD"
Units: mm.
Table 3.2216.0 GPS week: 2216 Day: 0 MJD: 59756.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 5 9 7 9 10 3 8 8 6 6 2 | 27 30 30 28 30 29 31 28 32 30 29
2 | 6 12 5 12 6 5 7 8 8 7 2 | 28 28 29 30 27 29 31 27 27 31 28
3E | 6 11 5 9 12 4 7 7 8 10 3 | 32 34 33 31 33 33 34 33 34 34 32
4 | 8 14 5 8 10 3 11 6 7 7 3 | 69 72 67 69 65 69 70 68 70 68 68
5E | 7 11 8 14 9 4 8 6 8 9 3 | 56 59 57 55 59 58 59 58 59 57 57
6 | 5 15 7 10 7 3 8 5 10 7 2 | 32 33 33 32 30 32 35 30 31 34 31
7 | 9 10 6 7 7 3 7 7 7 7 2 | 41 45 43 44 46 42 45 43 45 41 43
8 | 8 9 7 9 12 4 8 6 8 9 3 | 513 420 420 422 262 514 424 419 419 424 514
9 | 7 9 7 7 9 3 6 7 7 7 2 | 22 26 23 22 25 24 28 23 23 24 23
10E | 8 9 7 10 13 5 7 7 12 11 3 | 38 40 39 43 42 39 40 41 41 43 40
11 | 9 14 19 12 10 6 9 7 9 8 4 | 51 53 47 55 55 51 54 54 54 56 52
12 | 5 17 10 11 10 4 7 7 7 7 3 | 42 45 37 44 41 41 45 45 44 44 42
13 | 4 8 10 9 9 5 9 7 12 7 3 | 36 40 36 37 35 37 43 36 39 39 37
14 | 12 19 9 18 11 6 10 23 13 14 5 | 83 77 78 85 79 80 79 75 84 83 80
15 | 8 10 7 12 11 5 6 9 10 8 3 | 57 58 57 58 55 56 57 55 52 54 56
16 | 18 30 8 20 22 8 11 14 11 16 5 | 35 38 32 34 33 33 34 37 34 38 33
17 | 7 13 8 10 7 5 8 6 9 6 3 | 34 33 27 35 32 31 32 33 33 32 32
18 | 10 16 13 13 10 6 8 8 8 10 3 | 61 60 58 63 62 59 60 59 59 63 59
19 | 6 21 9 8 8 7 10 9 8 8 3 | 37 42 36 37 37 37 38 39 37 37 37
20E | 13 10 6 14 8 6 7 11 12 7 3 | 61 62 62 65 61 63 63 63 61 61 61
21 | 5 13 7 8 12 5 6 8 7 5 2 | 27 29 27 28 26 27 30 27 31 28 27
22 | 4 15 7 12 8 4 5 5 9 6 2 | 29 35 28 34 31 30 30 30 33 30 30
23E | 10 25 11 28 19 7 12 12 17 9 5 | 37 37 42 49 40 41 41 40 38 39 38
24 | 9 11 6 16 7 5 10 8 8 8 3 | 28 36 31 41 28 32 36 28 31 32 31
X25 | 5 --- 6 15 10 5 10 11 7 7 3 | 30 --- 31 32 28 28 30 31 28 30 29
26 | 8 11 8 9 11 4 9 9 10 16 3 | 42 39 41 44 41 40 40 42 39 42 41
27 | 9 15 8 11 10 3 8 12 7 7 3 | 35 40 37 38 36 35 36 37 38 36 36
X28 | 8 11 10 14 18 8 10 11 9 --- 4 | 50 51 53 53 50 53 46 52 53 --- 52
29 | 6 19 7 8 9 6 9 6 9 9 3 | 43 43 42 45 40 42 43 42 42 42 42
30 | 8 10 8 10 7 4 9 6 9 9 3 | 28 31 28 28 26 29 34 27 30 26 28
31 | 5 7 6 10 8 5 7 5 7 9 2 | 41 45 45 40 44 44 45 45 43 42 43
32 | 5 16 8 9 10 4 9 8 8 6 3 | 23 33 25 23 23 24 28 25 23 24 24
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 14 8 12 11 5 8 9 9 9 |T 55 55 52 54 47 55 54 52 53 53 55
WRMS | 8 14 8 12 9 5 8 8 9 8 |NE 67 65 61 63 51 67 63 62 62 64 67
MEDI | 7 12 7 10 10 5 8 7 8 8 |MD 37 40 37 40 37 37 40 39 38 39 37
Table 3.2216.1 GPS week: 2216 Day: 1 MJD: 59757.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 5 10 7 11 10 4 8 7 7 7 2 | 30 30 32 35 32 30 30 30 31 29 30
2 | 5 9 6 12 8 3 11 7 7 6 2 | 30 30 31 34 29 30 33 29 30 30 30
3E | 7 10 6 8 15 2 9 3 9 8 3 | 47 46 48 48 49 48 46 47 49 47 47
4 | 7 15 5 11 9 3 11 4 6 7 2 | 55 54 52 59 51 53 54 55 54 54 54
5E | 7 11 8 9 10 4 11 5 12 8 3 | 69 69 71 71 71 69 70 69 70 71 70
6 | 5 11 6 8 9 3 7 8 7 5 2 | 28 31 30 29 27 29 32 26 29 29 28
7 | 4 6 6 9 5 4 8 6 6 6 2 | 42 41 42 49 41 44 43 39 39 40 41
8 | 9 11 7 13 12 3 8 4 8 6 3 | 581 470 470 467 272 580 469 467 467 469 581
9 | 4 9 7 10 10 4 7 7 6 8 2 | 35 36 34 35 33 35 37 33 34 35 34
10E | 8 11 6 11 11 5 9 7 13 9 3 | 48 52 48 52 52 48 47 50 47 50 49
11 | 7 12 18 16 12 5 11 7 7 8 4 | 33 37 34 40 36 35 40 34 35 35 35
12 | 6 18 9 13 10 4 9 5 6 8 3 | 43 44 43 45 41 42 44 43 43 44 43
13 | 6 12 8 8 12 5 9 6 7 9 3 | 42 47 43 44 45 43 48 42 43 45 44
14 | 9 16 8 12 12 7 11 14 11 11 4 | 57 56 56 56 56 58 58 52 57 56 55
15 | 7 11 6 10 10 5 7 8 8 7 2 | 51 54 52 54 49 52 53 51 49 47 51
16 | 14 24 8 15 19 4 13 9 8 12 4 | 38 38 37 41 42 36 37 39 40 38 37
17 | 7 13 9 9 9 4 7 9 9 6 3 | 28 28 25 31 28 28 29 28 28 29 27
18 | 10 15 15 11 11 5 11 5 7 11 3 | 35 37 37 36 35 33 37 34 32 37 34
19 | 6 18 9 12 9 4 10 9 9 8 3 | 25 28 27 27 26 26 28 27 26 27 26
20E | 18 15 5 25 13 7 13 11 25 13 5 | 50 53 50 55 52 51 55 50 54 52 50
21 | 6 12 8 9 19 5 9 6 11 6 3 | 29 29 31 33 34 29 30 29 30 28 29
22 | 6 9 7 10 9 3 7 3 5 8 2 | 41 42 41 44 40 42 40 41 42 40 41
23E | 11 21 10 27 16 8 13 10 16 11 5 | 55 59 56 59 55 55 56 56 55 57 55
24 | 7 11 6 17 8 5 11 5 7 9 3 | 31 40 38 46 31 36 41 33 33 33 35
25 | 7 11 8 10 11 4 10 9 7 7 3 | 30 28 32 30 30 31 33 30 30 32 30
26 | 8 10 7 8 14 4 11 8 9 8 3 | 43 46 44 45 47 43 43 43 42 42 43
27 | 10 10 10 9 9 3 9 8 8 9 3 | 48 47 46 49 46 45 46 47 46 47 46
X28 | 9 9 9 12 15 5 10 8 9 --- 3 | 32 30 29 32 30 30 33 32 34 --- 30
29 | 5 16 7 6 9 5 10 5 8 9 3 | 34 34 32 35 33 32 34 35 33 33 33
30 | 5 10 8 9 7 4 11 7 6 8 2 | 33 37 35 38 32 35 41 32 33 31 34
31 | 7 9 7 10 8 4 10 4 7 7 2 | 49 53 52 50 52 51 51 50 52 48 50
32 | 5 10 8 9 11 4 9 7 7 8 3 | 36 43 38 37 35 38 40 37 36 36 37
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 8 13 8 12 11 4 10 7 9 8 |T 57 55 54 56 47 57 55 53 53 54 57
WRMS | 7 13 8 14 10 4 10 7 8 8 |NE 67 61 61 63 49 67 62 60 61 63 67
MEDI | 7 11 7 10 10 4 10 7 7 8 |MD 38 41 38 44 40 38 41 39 39 40 37
Table 3.2216.2 GPS week: 2216 Day: 2 MJD: 59758.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 5 8 6 9 10 4 6 5 10 5 2 | 20 23 22 23 23 20 23 19 23 20 20
2 | 5 11 7 10 7 4 7 5 9 5 2 | 21 24 25 22 21 22 24 22 23 23 22
3E | 6 10 7 12 15 4 9 4 10 9 3 | 27 28 26 28 33 26 27 25 26 28 26
4 | 6 14 4 10 8 4 11 5 6 6 2 | 52 49 52 57 51 53 51 54 51 56 52
5E | 5 12 10 9 7 4 9 4 9 10 3 | 45 43 46 43 46 44 44 44 41 43 43
6 | 5 15 9 8 8 3 7 5 10 7 2 | 26 30 27 24 25 24 28 21 23 22 24
7M | 7 10 8 8 5 6 5 4 6 7 2 | 26 31 24 27 30 25 28 28 30 26 27
X8 | 14 29 15 12 --- 5 31 9 12 10 6 | 753 734 734 729 --- 753 733 733 732 733 754
9 | 7 9 7 9 8 5 5 6 6 8 2 | 21 27 24 23 24 23 28 24 22 25 23
10E | 7 12 7 11 17 6 8 10 13 8 3 | 32 32 34 35 36 33 35 36 34 32 33
11 | 8 13 18 15 10 7 10 7 8 9 4 | 34 38 36 38 38 35 38 38 32 39 36
12 | 5 15 10 11 9 6 7 4 8 6 3 | 28 27 24 26 30 27 27 27 28 29 26
13M | 5 10 7 9 8 4 9 4 8 8 2 | 24 30 26 25 24 26 33 24 25 25 25
14M | 10 19 10 17 10 5 11 9 9 12 4 | 53 49 49 55 52 50 50 46 48 54 50
15 | 6 10 6 13 7 5 5 5 7 9 2 | 44 43 39 41 42 42 43 44 40 41 42
16 | 11 26 6 21 16 8 11 11 8 16 4 | 25 26 24 26 24 22 23 26 24 29 23
17 | 7 13 10 9 10 5 7 7 9 7 3 | 22 22 19 25 24 21 23 23 24 25 22
18 | 10 15 14 11 9 6 10 5 9 10 3 | 44 41 40 43 43 41 43 41 40 45 41
19 | 6 18 10 9 10 5 8 7 10 8 3 | 21 25 21 23 24 21 22 22 22 24 21
20E | 18 17 9 8 11 10 16 11 26 12 5 | 62 58 56 57 58 57 56 58 62 58 57
21 | 7 8 7 10 13 5 7 6 10 8 3 | 15 20 16 19 22 16 20 18 17 21 16
22 | 5 11 5 14 7 2 7 4 5 8 2 | 19 21 19 28 18 21 21 18 22 20 19
23E | 9 21 11 26 17 9 12 10 15 11 5 | 29 31 33 35 31 29 33 31 31 28 29
24 | 7 11 6 16 8 4 9 5 8 7 3 | 20 31 23 35 19 24 30 20 23 20 22
25 | 6 12 6 11 9 4 9 8 9 8 3 | 22 26 22 21 21 20 22 21 18 25 20
26 | 7 10 8 10 10 5 8 8 11 10 3 | 37 36 35 36 37 35 35 36 34 36 35
27 | 6 15 8 8 9 4 8 8 8 7 3 | 28 29 33 27 27 28 30 26 28 28 27
X28 | 9 11 10 9 8 7 8 7 14 --- 3 | 34 30 27 32 30 27 25 32 34 --- 30
29 | 8 20 10 11 9 5 7 5 8 9 3 | 25 25 24 27 24 24 23 23 23 26 23
30M | 8 11 9 9 6 4 9 4 6 8 2 | 22 28 22 21 20 21 29 17 19 18 20
31 | 3 7 7 9 6 5 6 4 8 5 2 | 33 34 32 32 34 33 35 33 30 31 32
32 | 4 11 7 11 9 3 7 5 5 6 2 | 23 27 21 24 21 22 26 19 20 21 21
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 14 9 12 10 5 9 7 10 9 |T 52 53 51 53 30 52 53 51 51 53 51
WRMS | 7 14 9 11 9 5 9 6 9 8 |NE 72 72 70 71 27 71 71 70 70 75 71
MEDI | 7 12 8 10 9 5 8 5 9 8 |MD 26 30 26 27 27 26 28 26 26 28 26
Table 3.2216.3 GPS week: 2216 Day: 3 MJD: 59759.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 4 8 7 8 10 4 6 5 7 5 2 | 22 22 24 26 26 23 24 24 25 23 23
2 | 5 11 5 7 8 3 6 5 9 6 2 | 21 22 22 22 20 21 22 23 23 21 21
X3E | 6 --- 7 9 16 3 8 4 7 7 3 | 18 --- 18 23 24 18 20 17 17 19 18
4M | 7 12 5 9 11 3 11 5 6 7 2 | 38 38 35 41 36 38 38 38 36 41 37
5E | 6 9 8 9 26 5 8 6 8 4 3 | 30 29 29 27 36 29 28 31 30 31 29
6 | 5 9 7 7 8 4 7 5 7 6 2 | 24 25 24 22 21 22 26 20 22 22 22
7 | 7 9 4 8 6 4 5 3 8 10 2 | 48 49 48 51 49 49 50 48 54 49 49
8 | 11 10 6 9 20 4 8 5 10 8 3 | 506 604 602 604 620 506 606 603 601 607 505
9M | 5 9 7 6 9 4 7 3 5 7 2 | 21 23 22 21 22 20 24 20 22 20 21
10E | 9 11 6 12 15 4 9 8 12 13 3 | 24 27 25 27 27 27 25 29 26 32 25
11 | 8 13 18 12 11 5 8 6 9 12 4 | 41 43 39 44 44 40 41 43 42 42 41
12 | 7 16 8 9 9 4 7 5 8 6 3 | 25 24 22 25 26 25 25 24 25 25 23
13 | 5 11 8 10 10 5 9 7 9 9 3 | 21 29 21 20 21 22 27 21 19 22 21
14 | 10 19 11 14 11 4 10 7 11 9 4 | 56 51 50 58 53 54 53 50 54 56 52
15M | 7 8 6 10 9 5 7 7 8 12 3 | 50 49 48 48 47 49 52 47 51 46 48
16 | 11 27 7 13 16 5 10 13 5 13 4 | 23 25 22 24 24 20 22 24 22 25 21
17 | 6 9 9 8 9 3 7 6 7 10 2 | 26 28 24 30 25 26 27 26 25 30 26
18 | 9 15 16 11 11 7 10 6 11 11 4 | 49 47 45 46 46 46 48 50 48 49 47
19 | 5 13 9 6 9 4 7 6 5 6 2 | 25 29 25 29 27 26 26 26 27 29 26
20E | 7 16 7 13 7 6 13 6 17 8 3 | 30 31 33 34 33 33 33 33 34 30 31
21 | 6 12 5 6 13 4 7 6 9 6 2 | 18 22 19 22 22 19 20 19 20 20 18
22M | 6 9 5 9 10 2 7 6 8 8 2 | 16 20 16 22 16 16 18 17 18 19 16
23E | 8 20 10 24 19 8 14 11 14 15 5 | 38 36 39 47 36 37 37 41 33 43 37
24M | 9 10 5 11 9 4 9 7 9 9 3 | 19 31 24 31 20 24 31 21 19 22 23
25 | 6 10 8 11 11 3 8 8 9 9 3 | 22 27 24 19 23 23 25 22 22 25 21
26 | 7 8 8 6 13 4 7 10 10 10 3 | 20 19 24 21 21 21 23 22 20 25 21
27 | 8 18 8 9 12 4 7 11 7 7 3 | 45 47 45 44 42 43 44 43 41 44 43
X28 | 8 10 9 18 11 11 7 6 12 --- 4 | 26 24 21 23 23 21 23 23 27 --- 22
29 | 7 17 6 8 9 4 7 6 9 7 3 | 21 24 21 22 22 22 22 23 21 25 21
30 | 6 10 6 7 7 3 9 4 8 8 2 | 25 31 25 26 23 26 31 22 28 23 25
31M | 4 8 9 6 7 4 6 5 7 9 2 | 36 36 40 38 38 37 38 36 35 37 37
32M | 5 9 6 10 8 2 6 6 6 8 2 | 69 70 69 69 67 68 70 66 70 67 68
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 8 10 12 4 8 7 9 9 |T 45 51 48 50 49 45 49 48 48 50 44
WRMS | 7 13 8 11 10 4 8 6 8 8 |NE 57 64 62 63 64 56 64 63 63 67 56
MEDI | 7 10 7 9 10 4 7 6 8 8 |MD 25 29 24 27 26 26 27 24 26 29 25
Table 3.2216.4 GPS week: 2216 Day: 4 MJD: 59760.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 4 9 7 11 11 4 7 4 11 10 2 | 17 21 19 23 22 17 18 17 19 21 17
2 | 6 10 4 10 7 3 6 4 6 6 2 | 16 19 19 23 18 18 19 18 19 19 17
3E | 7 9 7 37 13 5 8 4 14 11 4 | 19 27 22 29 26 21 23 21 24 22 20
4 | 5 12 5 7 9 4 9 4 10 7 2 | 41 40 40 41 39 41 41 42 42 41 40
5E | 5 11 8 12 10 4 6 5 11 8 3 | 45 45 44 41 45 43 44 43 43 43 43
6 | 4 7 7 8 7 3 6 4 7 7 2 | 21 23 24 22 20 21 24 19 22 22 21
7 | 5 9 5 11 7 3 6 3 6 8 2 | 63 64 65 67 65 64 65 65 63 65 64
X8 | 1 --- --- --- --- 17 --- --- --- --- 0 | 17 --- --- --- --- 20 --- --- --- --- 18
9 | 4 9 6 8 8 4 7 3 8 7 2 | 19 22 19 19 19 18 22 19 18 19 18
10E | 8 13 6 23 12 4 8 8 14 12 4 | 27 31 28 39 32 30 30 29 28 35 29
11 | 6 13 17 17 11 5 10 7 8 11 3 | 32 37 31 39 39 32 35 35 34 34 33
12 | 6 13 8 11 11 5 8 4 8 7 2 | 29 28 26 28 28 26 26 29 28 29 27
13 | 6 11 7 16 8 4 10 4 6 11 3 | 24 28 23 20 22 23 30 23 23 25 23
14 | 10 18 11 18 10 6 11 6 12 12 4 | 46 44 41 48 44 45 46 46 46 49 44
15 | 7 9 5 12 7 5 6 5 9 9 2 | 43 44 40 42 41 40 42 42 40 40 41
16 | 10 24 8 10 17 5 8 9 7 11 4 | 20 23 20 20 24 19 20 24 21 24 20
17 | 6 10 7 10 9 5 6 5 10 8 2 | 21 20 17 24 22 20 22 22 21 25 20
18 | 8 15 14 12 11 6 10 8 8 11 3 | 35 39 35 38 39 35 39 40 41 42 37
19 | 5 14 7 13 10 5 7 5 6 9 2 | 20 21 21 21 21 20 21 23 19 27 21
20E | 6 12 5 12 12 4 10 6 16 8 3 | 43 43 42 41 43 42 43 43 45 43 42
21 | 5 13 7 13 14 5 8 6 12 10 3 | 14 20 17 21 20 15 17 17 19 20 16
22 | 4 8 6 13 8 2 6 4 10 7 2 | 18 20 16 25 18 18 19 18 21 20 18
23E | 7 21 13 24 22 9 13 14 21 21 5 | 24 26 26 28 31 25 28 29 28 33 25
24 | 6 12 6 15 8 4 10 5 9 10 3 | 31 36 31 39 29 30 37 30 29 32 31
25 | 8 11 7 10 8 3 10 6 9 8 3 | 20 23 22 18 21 18 20 19 16 20 18
26 | 7 10 7 9 13 4 8 7 8 9 3 | 28 27 28 28 26 27 26 29 24 29 26
27 | 6 16 9 12 10 4 10 5 7 6 3 | 24 28 27 23 27 25 26 23 25 23 24
X28 | 7 10 9 40 10 9 9 5 11 --- 4 | 30 29 25 52 26 27 23 28 30 --- 28
29 | 5 17 7 10 7 5 8 5 8 7 2 | 24 22 23 23 23 23 23 24 25 24 22
30 | 5 11 6 9 7 3 10 5 5 9 2 | 23 32 25 26 24 25 33 23 23 26 25
31 | 5 9 7 9 6 3 5 4 7 6 2 | 62 63 64 63 63 63 63 65 61 65 63
32 | 4 9 7 12 11 3 7 5 7 8 2 | 200 201 200 201 201 200 201 201 199 200 200
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 6 13 8 14 11 4 8 6 10 10 |T 34 36 34 37 36 34 36 35 35 37 34
WRMS | 6 13 8 13 9 4 8 5 9 8 |NE 23 25 23 26 25 22 23 24 24 25 22
MEDI | 6 11 7 12 10 4 8 5 8 8 |MD 24 28 26 28 26 25 26 28 25 27 25
Table 3.2216.5 GPS week: 2216 Day: 5 MJD: 59761.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 5 8 6 12 10 3 5 4 7 6 2 | 25 30 30 30 27 27 27 26 30 29 27
2 | 5 8 5 9 9 2 6 6 8 5 2 | 26 30 31 32 26 29 28 26 28 29 27
3E | 9 11 8 23 13 4 6 7 10 12 3 | 17 23 16 18 19 15 17 17 16 19 16
4 | 5 13 5 7 9 2 10 5 7 7 2 | 44 48 45 48 45 45 45 45 46 47 45
5E | 7 9 8 12 17 6 5 7 8 9 3 | 38 38 38 38 42 38 38 38 37 38 37
6 | 5 9 6 7 7 3 6 5 7 7 2 | 32 33 33 33 30 32 33 29 34 30 31
7 | 6 7 3 8 5 3 5 4 8 8 2 | 82 83 82 85 82 83 82 84 82 82 82
X8 | 11 8 5 14 14 4 6 7 9 --- 3 | 22 24 25 24 27 22 24 22 23 --- 23
9 | 6 8 6 7 7 3 7 5 9 7 2 | 24 26 26 25 24 25 28 23 26 23 24
10E | 7 12 8 23 14 7 8 12 13 12 4 | 26 24 25 38 27 25 25 27 26 31 26
11 | 8 12 17 13 12 5 8 9 7 13 4 | 36 39 38 42 39 36 38 37 36 40 37
12 | 4 16 9 16 11 4 7 6 8 8 3 | 30 30 25 33 27 27 28 29 28 33 28
13 | 5 9 6 15 8 4 8 5 7 7 2 | 19 25 20 18 18 20 28 19 18 19 20
14 | 11 19 11 19 11 5 10 7 12 9 4 | 50 46 46 53 49 48 48 49 51 49 48
15 | 7 7 6 13 8 4 7 8 7 8 2 | 36 35 32 35 32 33 35 35 34 37 34
16 | 11 28 7 13 17 5 11 14 7 13 4 | 19 28 20 21 24 20 19 27 22 25 20
17 | 6 11 8 9 8 5 8 7 9 8 3 | 32 33 32 37 31 33 33 31 37 34 32
18 | 7 13 15 13 10 8 9 9 6 13 3 | 37 42 38 36 40 37 41 41 38 45 39
19 | 6 16 8 8 10 5 8 5 9 8 3 | 28 32 29 32 31 29 29 29 34 33 30
20E | 9 11 6 12 11 3 9 7 8 8 3 | 26 26 29 29 29 27 26 31 29 30 27
21 | 6 10 7 13 14 5 7 6 10 8 3 | 20 25 23 27 25 21 22 22 22 23 21
22 | 3 11 7 11 9 4 4 6 7 6 2 | 14 20 13 19 16 15 17 16 15 15 15
23E | 7 19 12 22 17 9 15 15 20 25 6 | 28 28 30 35 30 27 28 32 26 38 27
24 | 6 10 4 17 10 3 8 6 8 6 2 | 39 45 41 49 38 41 45 38 39 38 40
25 | 6 10 7 14 9 3 7 8 7 6 2 | 26 30 28 24 26 25 27 27 25 29 26
26 | 9 8 8 11 12 4 9 11 10 13 3 | 35 34 37 38 35 35 36 37 37 37 35
27 | 10 14 8 15 12 4 8 13 9 9 3 | 27 34 30 29 28 27 27 29 26 26 27
X28 | 7 8 7 14 9 5 10 6 10 --- 3 | 34 35 35 33 34 34 28 33 35 --- 34
29 | 5 16 7 10 6 5 7 7 7 7 2 | 29 30 27 28 29 28 28 30 31 30 28
30 | 7 10 5 8 7 3 10 4 8 10 2 | 20 29 22 23 17 22 29 18 22 20 21
31 | 5 9 7 6 6 4 6 5 8 8 2 | 83 81 83 85 82 83 83 84 84 82 83
32 | 4 9 8 11 11 5 6 6 6 6 2 | 350 352 350 349 352 352 351 349 348 350 350
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 8 13 11 5 8 8 9 10 |T 42 44 43 45 43 42 43 43 43 45 42
WRMS | 7 13 8 13 10 4 8 6 8 7 |NE 28 31 30 31 29 28 29 29 30 31 29
MEDI | 6 10 7 12 10 4 7 6 8 8 |MD 28 30 30 33 29 28 28 29 30 31 28
Table 3.2216.6 GPS week: 2216 Day: 6 MJD: 59762.000
Weighted Average Orbit Dynamics (7 days)
PRN | cod emr esa gfz grg igr jpl mit ngs sio IGS | cod emr esa gfz grg igr jpl mit ngs sio IGS
------+--------------------------------------------------------+---------------------------------------------------------
1 | 5 8 7 11 8 3 7 4 8 10 2 | 27 30 28 30 28 27 29 27 31 33 28
2 | 6 11 5 11 8 2 7 4 11 8 2 | 26 31 30 33 25 29 29 28 29 31 28
3E | 8 10 10 28 12 6 8 5 15 10 4 | 51 54 54 55 58 53 52 54 59 56 54
4 | 4 12 7 7 9 4 9 5 8 7 2 | 68 71 69 72 68 70 69 70 72 70 69
5E | 10 13 9 10 13 7 9 10 10 14 3 | 76 79 80 79 78 79 79 78 75 80 77
6 | 5 11 7 8 7 3 6 3 4 9 2 | 30 35 33 32 29 31 34 29 32 31 31
7 | 5 9 5 6 6 2 5 3 7 6 2 | 140 140 139 141 139 140 140 140 142 140 140
8 | 9 11 7 11 14 3 8 5 9 8 3 | 25 23 24 24 27 25 24 21 24 14 24
9 | 5 9 6 7 8 3 7 5 7 7 2 | 35 40 39 40 37 38 40 38 41 39 37
10E | 8 17 6 21 12 4 8 12 14 10 4 | 56 60 57 64 59 58 56 57 60 59 57
11 | 9 13 18 14 10 4 9 7 7 9 3 | 56 59 54 62 59 56 57 58 57 59 57
12 | 6 15 8 8 11 5 7 5 8 8 3 | 38 41 39 39 37 39 39 38 37 39 37
13 | 5 10 7 13 8 4 10 5 7 5 2 | 33 41 35 36 35 35 42 34 36 36 35
14 | 8 19 13 14 12 4 12 7 12 10 4 | 60 56 56 66 61 61 60 60 63 62 59
15 | 6 10 5 11 8 4 6 7 6 7 2 | 64 69 66 68 65 66 67 65 65 65 65
16 | 9 24 7 9 15 5 8 11 6 12 4 | 30 26 30 31 34 27 27 31 29 29 28
17 | 7 10 7 7 10 6 9 7 5 8 2 | 27 33 26 33 29 28 30 30 29 32 28
18 | 9 12 16 11 11 5 10 8 9 9 3 | 62 62 59 64 62 61 60 63 65 65 62
19 | 6 12 7 7 11 5 8 5 5 11 2 | 28 34 28 31 29 28 31 30 28 34 29
20E | 6 13 6 20 8 2 11 5 8 6 3 | 45 49 49 51 47 46 49 46 50 45 47
21 | 7 10 8 17 14 4 8 6 11 9 3 | 22 29 23 28 27 23 26 25 27 29 24
22 | 7 9 7 9 11 4 7 5 9 9 2 | 32 36 34 38 34 34 34 33 35 34 33
23E | 12 18 17 22 27 10 23 20 12 38 7 | 45 51 47 50 46 46 47 56 53 65 48
24 | 5 13 7 7 6 4 13 6 9 7 3 | 53 63 56 58 52 56 59 54 54 54 55
25 | 6 13 8 13 9 5 8 9 9 9 3 | 27 37 29 30 30 29 31 25 28 28 27
26 | 9 12 11 13 12 5 10 10 10 6 3 | 89 88 93 92 84 88 89 89 93 90 89
27 | 9 14 9 12 11 3 10 9 9 10 3 | 29 30 34 28 28 28 29 28 26 32 28
X28 | 6 10 6 15 9 6 --- 8 10 --- 3 | 30 31 27 32 31 28 --- 30 30 --- 28
29 | 6 16 7 10 8 5 8 6 10 9 3 | 32 33 27 35 31 30 29 30 34 31 30
30 | 4 12 5 7 7 3 11 4 7 8 2 | 39 47 41 42 39 42 48 38 40 39 40
31 | 8 8 7 8 7 3 6 5 8 8 2 | 100 103 103 102 102 102 103 101 99 101 101
32 | 7 9 6 10 13 4 8 5 6 6 2 | 495 497 496 496 493 497 496 494 495 494 495
------+--------------------------------------------------------+---------------------------------------------------------
RMS | 7 13 9 13 11 4 9 7 9 11 |T 61 64 62 65 62 62 64 62 63 65 62
WRMS | 7 13 8 12 10 4 9 6 9 8 |NE 36 38 36 39 36 36 37 36 37 38 36
MEDI | 6 12 7 11 10 4 8 5 8 9 |MD 38 41 39 40 37 39 47 38 40 39 37
Table 4: Precise Navigation Summary.
Weekly station RMS w.r.t. the estimated coordinates for the Latitude,
Longitude and Height components. See Table 5 for the daily summary.
CLK - Satellite clocks used.
EPO - Mean number of satellite clock epochs available in the daily
solutions.
Units: mm.
Table 4.2216 GPS week: 2216 MJD: 59756.0-59762.0
CENT| CLK EPO | BRUX | TOW2 | YELL |
----+----------+-------------------+-------------------+-------------------+
cod | cod 3058 |U 11 10 27 |U 8 15 34 |U 0 0 0 |
emr | emr 3030 |U 18 16 38 |U 13 20 46 |U 0 0 0 |
esa | esa 3058 | 10 11 28 |U 8 16 39 | 0 0 0 |
gfz | gfz 3046 |U 9 11 29 |U 8 11 40 |U 0 0 0 |
grg | grg 3041 |U 11 11 28 |U 8 10 41 |U 0 0 0 |
igr | igr 3057 | 10 10 22 | 7 14 33 | 0 0 0 |
igs | igs 3056 | 10 10 24 | 7 13 33 | 0 0 0 |
jpl | jpl 3044 |U 13 13 29 |U 9 20 36 | 0 0 0 |
mit | mit 3058 |U 10 10 26 |U 8 12 33 |U 0 0 0 |
Table 5: Daily Precise Navigation Summary using the corresponding Centre orbit
positions and satellite clock corrections at 15 min intervals.
Each line gives the daily station RMS w.r.t. the estimated coordinates
for the Latitude, Longitude and Height components.
CLK - Satellite clocks used.
EPO - Number of satellite clock epochs available for that day.
Units: mm.
Table 5.2216.0 GPS week: 2216 Day: 0 MJD: 59756.0
CENT| CLK EPO | BRUX | TOW2 |
----+----------+-------------------+-------------------+
cod | cod 3072 | 14 11 35 | 6 17 42 |
emr | emr 2976 | 20 10 42 | 10 23 36 |
esa | esa 3072 | 10 11 29 | 6 19 47 |
gfz | gfz 3072 | 10 11 36 | 8 13 40 |
grg | grg 3072 | 12 10 38 | 9 12 43 |
igr | igr 3072 | 11 11 29 | 5 14 37 |
igs | igs 3072 | 11 10 30 | 5 15 37 |
jpl | jpl 3072 | 13 12 32 | 6 22 38 |
mit | mit 3072 | 12 11 32 | 8 14 40 |
Table 5.2216.1 GPS week: 2216 Day: 1 MJD: 59757.0
CENT| CLK EPO | BRUX | TOW2 |
----+----------+-------------------+-------------------+
cod | cod 3072 | 11 13 28 | 5 17 30 |
emr | emr 3072 | 13 16 36 | 12 20 49 |
esa | esa 3072 | 9 16 28 | 8 18 36 |
gfz | gfz 3067 | 11 22 35 | 7 11 28 |
grg | grg 3062 | 10 17 34 | 7 9 44 |
igr | igr 3072 | 10 13 24 | 6 13 28 |
igs | igs 3064 | 9 13 26 | 6 14 30 |
jpl | jpl 3072 | 11 13 31 | 9 21 34 |
mit | mit 3072 | 10 13 28 | 6 13 29 |
Table 5.2216.2 GPS week: 2216 Day: 2 MJD: 59758.0
CENT| CLK EPO | BRUX | TOW2 |
----+----------+-------------------+-------------------+
cod | cod 3072 | 10 10 26 | 11 17 39 |
emr | emr 3072 | 22 17 33 | 15 24 44 |
esa | esa 3072 | 10 9 27 | 10 19 44 |
gfz | gfz 3071 | 8 8 25 | 10 17 47 |
grg | grg 2965 | 14 10 22 | 10 14 45 |
igr | igr 3072 | 12 11 18 | 9 20 42 |
igs | igs 3072 | 10 10 21 | 10 18 37 |
jpl | jpl 3072 | 17 19 27 | 12 26 42 |
mit | mit 3072 | 10 9 24 | 11 18 37 |
Table 5.2216.3 GPS week: 2216 Day: 3 MJD: 59759.0
CENT| CLK EPO | BRUX | TOW2 |
----+----------+-------------------+-------------------+
cod | cod 3070 | 9 9 32 | 8 11 32 |
emr | emr 2974 | 18 25 48 | 13 15 45 |
esa | esa 3072 | 10 11 35 | 8 11 37 |
gfz | gfz 3051 | 7 10 34 | 6 8 40 |
grg | grg 3070 | 12 10 29 | 8 9 36 |
igr | igr 3070 | 9 9 29 | 7 10 28 |
igs | igs 3070 | 9 9 30 | 7 9 30 |
jpl | jpl 3072 | 12 12 34 | 9 18 38 |
mit | mit 3072 | 8 9 29 | 8 9 27 |
Table 5.2216.4 GPS week: 2216 Day: 4 MJD: 59760.0
CENT| CLK EPO | BRUX | TOW2 |
----+----------+-------------------+-------------------+
cod | cod 2976 | 13 11 24 | 7 15 31 |
emr | emr 2976 | 19 14 36 | 12 20 48 |
esa | esa 2976 | 11 10 27 | 9 15 37 |
gfz | gfz 2921 | 11 8 27 | 7 10 47 |
grg | grg 2976 | 13 11 26 | 8 9 38 |
igr | igr 2973 | 12 11 18 | 7 13 31 |
igs | igs 2976 | 12 10 21 | 7 12 33 |
jpl | jpl 2976 | 15 14 25 | 8 19 36 |
mit | mit 2976 | 12 10 26 | 7 11 32 |
Table 5.2216.5 GPS week: 2216 Day: 5 MJD: 59761.0
CENT| CLK EPO | BRUX | TOW2 |
----+----------+-------------------+-------------------+
cod | cod 3072 | 10 9 25 | 7 12 33 |
emr | emr 3072 | 15 14 39 | 14 20 49 |
esa | esa 3072 | 10 11 26 | 7 15 35 |
gfz | gfz 3071 | 10 11 25 | 8 9 51 |
grg | grg 3072 | 9 11 26 | 8 8 38 |
igr | igr 3072 | 9 9 21 | 6 12 33 |
igs | igs 3072 | 8 9 22 | 6 11 34 |
jpl | jpl 3072 | 12 9 32 | 8 20 36 |
mit | mit 3072 | 8 10 24 | 7 10 32 |
Table 5.2216.6 GPS week: 2216 Day: 6 MJD: 59762.0
CENT| CLK EPO | BRUX | TOW2 |
----+----------+-------------------+-------------------+
cod | cod 3072 | 10 9 19 | 10 14 34 |
emr | emr 3072 | 20 16 31 | 14 20 52 |
esa | esa 3072 | 10 10 27 | 9 15 38 |
gfz | gfz 3071 | 8 9 21 | 8 10 29 |
grg | grg 3072 | 8 10 21 | 10 8 43 |
igr | igr 3072 | 9 10 16 | 9 13 31 |
igs | igs 3072 | 9 9 17 | 9 12 33 |
jpl | jpl 2976 | 12 11 25 | 8 18 31 |
mit | mit 3072 | 8 9 20 | 10 12 33 |
Table 6: Earth Orientation Parameters weekly summary.
Weekly mean and standard deviation of Centre ERP, ERP rates and
LOD differences with respect to IGS combined values. See Table 7 for
the daily summaries.
Xpole,Xrt: x pole and x pole rate
Ypole,Yrt: y pole and y pole rate
LOD : Length Of Day
AC LOD BIAS : 10-day mean LOD bias with respect to Bulletin A
AC LOD BIAS RMS: RMS of AC LOD BIAS
FLAG: "u" (used), "x" (excluded), "-" (no submission)
for Xpole, Ypole, Xrt, Yrt and LOD
Table 6.2216 GPS week: 2216 MJD: 59756.500-59762.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 10 -28 41 -58 1 | 8 26
| 20 19 34 58 4 | 3
emr uuuuu | -19 -14 -66 80 -6 | 10 29
| 26 17 88 86 8 | 3
esa uuuuu | 7 11 19 24 -1 | 11 24
| 10 13 46 21 2 | 2
gfz uuuuu | 2 7 -47 -143 5 | 23 32
| 22 29 133 112 5 | 3
grg uuuuu | -13 -2 -1 -121 -2 | 4 22
| 5 14 30 61 4 | 2
igr xxxxx | 12 -13 35 -18 3 | 2 21
| 8 9 74 40 6 | 3
irf xxxxx | 10 7 -5 3 1 | 1 22
| 6 9 25 24 4 | 3
jpl uuuuu | 11 -7 7 23 4 | 33 40
| 15 8 42 28 12 | 5
mit uuuuu | 3 30 -9 17 3 | 19 28
| 13 12 50 35 3 | 3
ngs uuxuu | -22 -6 59 126 0 | 11 23
| 20 36 232 98 4 | 2
sio xxxxx | -112 7 -93 6 -2 | 19 27
| 36 23 104 176 5 | 2
Table 7.2216.0 GPS week: 2216 Day: 0 MJD: 59756.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 17 -43 40 -107 -7 | 9 19
emr uuuuu | -26 13 -98 101 -16 | 16 25
esa uuuuu | -1 24 21 29 1 | 12 19
gfz uuuuu | -3 43 -169 -242 -1 | 25 29
grg uuuuu | -8 10 34 -159 2 | 6 17
igr xxxxx | 25 -8 96 39 9 | 1 15
irf xxxxx | 4 12 36 -31 2 | 1 16
jpl uuuuu | 21 -13 25 17 13 | 30 34
mit uuuuu | -15 25 26 44 5 | 19 24
ngs uuxuu | -3 -34 255 270 7 | 13 19
sio xxxxx | -115 29 25 -276 2 | 22 25
Table 7.2216.1 GPS week: 2216 Day: 1 MJD: 59757.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -1 7 74 -5 0 | 5 25
emr uuuuu | -16 -27 24 23 -13 | 11 30
esa uuuuu | 20 2 60 19 0 | 9 23
gfz uuuuu | 8 33 -242 -157 -3 | 20 30
grg uuuuu | -17 17 -2 -151 -3 | 2 22
igr xxxxx | 12 -11 143 -88 7 | -2 20
irf xxxxx | 10 9 -15 1 7 | -3 23
jpl uuuuu | 2 -13 24 -31 15 | 26 34
mit uuuuu | 9 20 -31 52 7 | 15 26
ngs uuxuu | -19 -49 315 125 -1 | 9 22
sio xxxxx | -144 39 -171 3 -11 | 18 27
Table 7.2216.2 GPS week: 2216 Day: 2 MJD: 59758.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 46 -22 -21 -165 3 | 6 26
emr uuuuu | -50 -16 9 166 -1 | 10 29
esa uuuuu | -6 25 74 26 -1 | 9 24
gfz uuuuu | 45 29 -145 43 6 | 20 30
grg uuuuu | -11 -2 -27 -27 -10 | 3 23
igr xxxxx | 5 2 -15 9 7 | -1 21
irf xxxxx | 5 21 8 20 4 | -1 23
jpl uuuuu | -14 -2 35 23 15 | 30 38
mit uuuuu | -9 20 9 15 2 | 16 27
ngs uuxuu | -21 -36 302 60 0 | 9 23
sio xxxxx | -61 10 -59 318 2 | 17 26
Table 7.2216.3 GPS week: 2216 Day: 3 MJD: 59759.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -6 -47 35 -33 0 | 8 28
emr uuuuu | -40 -28 13 -17 -8 | 10 29
esa uuuuu | 2 6 42 16 -6 | 10 25
gfz uuuuu | -18 2 62 -21 7 | 21 32
grg uuuuu | -11 8 23 -192 -2 | 4 23
igr xxxxx | 1 -13 -25 -33 3 | 2 23
irf xxxxx | 7 7 -43 -16 2 | 1 24
jpl uuuuu | 17 -15 1 15 6 | 33 42
mit uuuuu | 18 19 -112 2 4 | 18 29
ngs uuxuu | 9 53 -37 162 4 | 11 24
sio xxxxx | -140 -19 -119 -6 1 | 18 27
Table 7.2216.4 GPS week: 2216 Day: 4 MJD: 59760.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 15 -25 60 -16 2 | 9 27
emr uuuuu | -29 -14 -92 -18 -11 | 9 29
esa uuuuu | 5 -10 -50 58 0 | 10 25
gfz uuuuu | -13 -27 50 -220 11 | 23 32
grg uuuuu | -8 -13 -53 -63 -2 | 4 23
igr xxxxx | 16 -18 -68 -36 -3 | 4 22
irf xxxxx | 21 2 -20 43 2 | 2 24
jpl uuuuu | 8 -14 27 49 0 | 35 43
mit uuuuu | 15 42 3 56 6 | 19 29
ngs uuxuu | -41 22 -273 -43 -2 | 12 24
sio xxxxx | -141 13 -41 30 -6 | 18 27
Table 7.2216.5 GPS week: 2216 Day: 5 MJD: 59761.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | 12 -45 19 -47 2 | 10 27
emr uuuuu | 16 5 -100 107 7 | 7 30
esa uuuuu | 19 8 -32 -12 0 | 11 25
gfz uuuuu | 13 -25 74 -163 5 | 25 33
grg uuuuu | -14 -16 11 -166 -2 | 5 23
igr xxxxx | 19 -27 53 -17 -6 | 4 22
irf xxxxx | 16 8 -11 5 -3 | 3 23
jpl uuuuu | 7 6 24 52 -16 | 37 44
mit uuuuu | -6 51 -2 -12 2 | 20 29
ngs uuxuu | -45 4 -117 178 -3 | 12 24
sio xxxxx | -63 -9 -11 51 0 | 18 27
Table 7.2216.6 GPS week: 2216 Day: 6 MJD: 59762.500
AC LOD AC LOD
CENT FLAG | Xpole Ypole Xrt Yrt LOD | BIAS BIAS RMS
| [uas] [uas] [uas/d] [uas/d] [us]| [us] [us]
------------+----------------------------------------+------------------
cod uuuuu | -13 -25 76 -30 5 | 13 30
emr uuuuu | 15 -31 -218 197 -2 | 7 30
esa uuuuu | 13 19 20 31 -1 | 13 28
gfz uuuuu | -16 -6 40 -244 11 | 29 38
grg uuuuu | -21 -19 9 -90 0 | 7 25
igr xxxxx | 7 -20 59 0 3 | 7 24
irf xxxxx | 12 -9 7 -3 -5 | 5 25
jpl uuuuu | 35 0 -85 39 -5 | 39 45
mit uuuuu | 12 34 40 -37 -1 | 23 33
ngs uuxuu | -31 -5 -34 127 -4 | 14 27
sio xxxxx | -115 -17 -277 -77 0 | 19 29
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